問題一覧
1
Behind the nose radome
2
34.09m
3
Both FWD and AFT cargo compartment
4
Amber
5
DOOR
6
Temperature, G load, UTC and GW
7
PFD 1, ND 1, E/WD and SD
8
Once the crew has cleared all the pages corresponding to the current failure, or when the slats are extended (if failure still exists)
9
GEN 1, GEN 2, external power and APU GEN
10
No
11
To transform and rectify A/C power to D/C power
12
GEN 1 and GEN 2 have the highest priority on their own buses (AC bus 1 and 2)
13
Two Flight Management Guidance Computers (FMGC), Two Multipurpose Control and Display Unit (MCDU), One Flight Control Unit (FCU), and Two Flight Augmentation Computers (FAC)
14
200
15
#2
16
White
17
Flight Control Unit (FCU)
18
1500 ft RA
19
At least 2 seconds
20
Two independent receivers
21
2700 feet above / 2700 feet below the aircraft
22
2500 feet
23
Advisory message regarding APU oil level when aircraft is on the ground and APU not running
24
On ground only
25
APU FIRE handle and APU SHUT OFF p/b on the interphone panel under the nose fuselage
26
Bleed air is cooled by a pre-cooler, using cooling air bleed from the engine fan
27
Air conditioning, engine starting, water system pressurization, wing anti-icing and hydraulic reservoir pressurization
28
The HP valve opens and the IP stage remains in the same configuration
29
A zone controller and two pack controllers, or two Air Conditioning System Controllers (ACSC)
30
When a duct overheat or absence of pneumatic pressure exists
31
In the turbine
32
18-30 deg C
33
Yes, by selecting the YELLOW ELEC pump to ON, PTU switch to AUTO, and differential pressure > 500 psi
34
Priority valves cut off hydraulic power to heavy load users if hydraulic pressure in a system gets low
35
3000 psi, (2500 psi when powered by RAT)
36
Green and Yellow
37
Elevator and Aileron Computer (ELAC) and Spoiler and Elevator Computers (SEC)
38
Elevator and Aileron Computer (ELAC) 1
39
Spoilers 1-5
40
They are all electrically controlled and hydraulically activated
41
On top of the fuselage
42
37.57 m
43
Primary boxed, Secondary indicated by a star
44
AC BUS 1
45
V2 + 10 knots / Highest of V2 or current speed (Maximum V2 + 15 knots)
46
Dual mode
47
ADIRS 1 or 2 are not available or selected OFF, or the data from the ECB are invalid or not transmitted
48
When N > 95%
49
Two Bleed Monitoring Computers
50
The HP valve opens and the IP stage remains in the same configuration
51
Fully automatic
52
Close automatically
53
If AC BUS 1 and AC BUS 2 are both lost
54
Green and yellow
55
The bank angle goes to 67° and no further
B777 - Part 8
B777 - Part 8
Angelo Ortiz · 50問 · 3年前B777 - Part 8
B777 - Part 8
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B777 - Part 6
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B777 - Part 4
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B777 - Part 1
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B777 - Part 1
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B777 - Part 7
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B777 - Part 9
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B777 - Part 9
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B777 - Part 2
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B777 - Part 5
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B777 - Part 5
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Angelo Ortiz · 30問 · 2年前Navigation
Navigation
30問 • 2年前問題一覧
1
Behind the nose radome
2
34.09m
3
Both FWD and AFT cargo compartment
4
Amber
5
DOOR
6
Temperature, G load, UTC and GW
7
PFD 1, ND 1, E/WD and SD
8
Once the crew has cleared all the pages corresponding to the current failure, or when the slats are extended (if failure still exists)
9
GEN 1, GEN 2, external power and APU GEN
10
No
11
To transform and rectify A/C power to D/C power
12
GEN 1 and GEN 2 have the highest priority on their own buses (AC bus 1 and 2)
13
Two Flight Management Guidance Computers (FMGC), Two Multipurpose Control and Display Unit (MCDU), One Flight Control Unit (FCU), and Two Flight Augmentation Computers (FAC)
14
200
15
#2
16
White
17
Flight Control Unit (FCU)
18
1500 ft RA
19
At least 2 seconds
20
Two independent receivers
21
2700 feet above / 2700 feet below the aircraft
22
2500 feet
23
Advisory message regarding APU oil level when aircraft is on the ground and APU not running
24
On ground only
25
APU FIRE handle and APU SHUT OFF p/b on the interphone panel under the nose fuselage
26
Bleed air is cooled by a pre-cooler, using cooling air bleed from the engine fan
27
Air conditioning, engine starting, water system pressurization, wing anti-icing and hydraulic reservoir pressurization
28
The HP valve opens and the IP stage remains in the same configuration
29
A zone controller and two pack controllers, or two Air Conditioning System Controllers (ACSC)
30
When a duct overheat or absence of pneumatic pressure exists
31
In the turbine
32
18-30 deg C
33
Yes, by selecting the YELLOW ELEC pump to ON, PTU switch to AUTO, and differential pressure > 500 psi
34
Priority valves cut off hydraulic power to heavy load users if hydraulic pressure in a system gets low
35
3000 psi, (2500 psi when powered by RAT)
36
Green and Yellow
37
Elevator and Aileron Computer (ELAC) and Spoiler and Elevator Computers (SEC)
38
Elevator and Aileron Computer (ELAC) 1
39
Spoilers 1-5
40
They are all electrically controlled and hydraulically activated
41
On top of the fuselage
42
37.57 m
43
Primary boxed, Secondary indicated by a star
44
AC BUS 1
45
V2 + 10 knots / Highest of V2 or current speed (Maximum V2 + 15 knots)
46
Dual mode
47
ADIRS 1 or 2 are not available or selected OFF, or the data from the ECB are invalid or not transmitted
48
When N > 95%
49
Two Bleed Monitoring Computers
50
The HP valve opens and the IP stage remains in the same configuration
51
Fully automatic
52
Close automatically
53
If AC BUS 1 and AC BUS 2 are both lost
54
Green and yellow
55
The bank angle goes to 67° and no further